BLUNT BODY THEORY FOR HYPERSONIC FLOW

Abstract

A systematic analysis of Newtonian flow past an axi-symmetrical blunt body is developed by expanding various physical quantities in power series of lambda equals (gamma-1)/(gamma+1), where gamma stands for the ratio of specific heats of a gas. Some general results such as stand-off distance, pressure distribution along the axis of symmetry are given, provided that the shock is detached and has finite curvature at its nose. More extensive calculations are made for the flow past a flat-faced disc and power-law bodies. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1961
Accession Number
AD0262022

Entities

People

  • K. Hida

Organizations

  • California Institute of Technology

Tags

DTIC Thesaurus Topics

  • Blunt Bodies
  • Bodies
  • Curvature
  • Flow
  • Geometric Forms
  • Geometry
  • Hypersonic Flow
  • Power Series
  • Pressure Distribution
  • Specific Heat
  • Symmetry

Fields of Study

  • Physics

Readers

  • Explosive Engineering.
  • Fluid Mechanics and Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flight